Boeing 727-31C

Service difficulty reports · 885

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Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '72731C'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UPS97221924Fan Blades · bentWHILE PERFORMING WEEKEND CHECK, FOUND NR 3 ENGINE WITH (5) BENT FAN (N1) BLADE TIPS. FOUND NR 3 ENGINE FAN BLADE TIPS (5) WITHIN MM LIMITS AS PER 72-00 PR 616 A FIG 601 SHEET 3.Feb 3, 1997 · N923UP · Boeing 72731C · Turbine Engine Compressor SectionSDR UPS97221819Slat · crackedINSPECTION TYPE-N/A, NR 5 SLAT CRACKED AT OUTBOARD STOP THROUGH STOP MOUNTING POINTS. REPLACED NR 5 LEADING EDGE SLAT WITH A BORROWED PART FROM DELTA AIRLINES. WITH REF TO M/M 27-81-11. GRND CHKS GOOD. REMOVED (P/N 65-1 6221-2) (S/N BN46) OFF, (P/N 65-16221-Jan 12, 1997 · N922UP · Boeing 72731C · Leading Edge DevicesSDR UPS96221156Stiffener · crackedINSPECTION TYPE-C, RT WING NR 5 SLAT AT ACTUATOR ROD MOUNT STIFFENER IS CRACKED IN RADIUS. REPAIRED IAW SRM 51-40-03 AND SRM 51-30-02.Sep 8, 1996 · N925UP · Boeing 72731C · Wing Miscellaneous StructureSDR UPS96221155Ribs · crackedINSPECTION TYPE-C, RT WING NR 5 SLAT, OUTBD AND INBD ACTUATOR ATTACH RIBS ARE CRACKED. REMOVED RIBS AND FABRICATED REPLACEMENT RIBS IAW DWG 65-17276 AND INSTALLED IAW SRM 51-30-02.Sep 8, 1996 · N925UP · Boeing 72731C · Wing, Rib/BulkheadSDR UPS96221154Spar Chord · crackedINSPECTION TYPE-C, RT O/B AILERON UPPER SPAR CHORD IS CRACKED, JUST O/B OF THE CENTER I/B HINGE. FABBED AND INSTALLED REPLACEMENT PART IAW SRM 57-30-02 AND 51-30-2.Sep 8, 1996 · N925UP · Boeing 72731C · AileronsSDR UPS96221145Clip · crackedINSPECTION TYPE-C, BS 1070 AT STR 6L AND 5L STRINGER TO FRAME CLIPS CRACKED. REMOVED, FABRICATED AND INSTALLED NEW CLIPS IAW BAC DWG 65-45313 AND SRM 51-30-2.Sep 8, 1996 · N925UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS96221144Clip · crackedINSPECTION TYPE-C, BS 1070 STR 6R STRINGER TO FRAME CLIP CRACKED. REMOVED, FABRICATED AND INSTALLED NEW CLIP IAW DWG 65-45313 AND SRM 51-30-2.Sep 8, 1996 · N925UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS96221153Vert Stiffener · crackedINSPECTION TYPE-C, LT WING L/E, NR 3 SLAT I/B TRACK, O/B MOUNT VERTICAL STIFFENER ANGLE IS CRACKED AT BOTTOM. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW 65-16200 AND SRM 51-30-02.Sep 7, 1996 · N925UP · Boeing 72731C · Wing Miscellaneous StructureSDR UPS96221152Vert Stiffener · crackedINSPECTION TYPE-C, LT WING NR 3 SLAT O/B TRACK, O/B MOUNT VERTICAL STIFFENER ANGLE IS CRACKED AT BOTTOM. REMOVED DAMAGED STIFFENER, FAB AND INSTALLED REPLACEMENT STIFFENER SEALED DOME FASTENERS.Sep 7, 1996 · N925UP · Boeing 72731C · Wing Miscellaneous StructureSDR UPS96221151Vert Stiffener · crackedINSPECTION TYPE-C, LT WINGS L/E NR 2 SLAT I/B TRACK O/B MOUNT VERTICAL STIFFENER ANGLE IS CRACKED AT THE BOTTOM. REMOVED, FABRICATED AND INSTALLED STIFFENER ANGLE PER DWG 65-16200 SHT 1 AND 8 AND SRM 51-30-2.Sep 7, 1996 · N925UP · Boeing 72731C · Wing Miscellaneous StructureSDR UPS96221149Frame · bulgedINSPECTION TYPE-C, LT FUSELAGE IS BULGED AT FRAME BS 990 BETWEEN S17 AND S18L. REMOVED DAMAGED AREA, TREATED AND PRIMED, INSTALLED REPAIR AND REINSTALLED FAIRING ATTCH FITTING.Sep 7, 1996 · N925UP · Boeing 72731C · Fuselage Main, FrameSDR UPS96221146Channel · corrodedINSPECTION TYPE-C, U-CHANNEL DIRECTLY BELOW THE LAV DOOR IS CORRODED. REMOVED DAMAGED U-CHANNEL IAW SRM 51-10-01. FABRICATED U-CHANNEL IAW SRM 53-10-01 AND INSTALLED IAW SRM 51-10-01.Sep 6, 1996 · N925UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS96221150Web · crackedINSPECTION TYPE-C, AFT TORQUE BOX UPPER WEB AT BS 1270 IS CRACKED AT FASTENER IN THE INBD CHORD. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER.Sep 5, 1996 · N925UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS96221148Seal Retainer · corrodedINSPECTION TYPE-C, RT AFT NLG DOOR SEAL RETAINER CORRODED. REPLACED RT AFT NLG DOOR SEAL RETAINER PER SRM 51-30-2.Sep 5, 1996 · N925UP · Boeing 72731C · Landing Gear DoorsSDR UPS96221147Seal Retainer · corrodedINSPECTION TYPE-C, LT AFT NLG DOOR SEAL RETAINER CORRODED. REPLACED LT AFT NLG DOOR SEAL RETAINER PER SRM 51-30-02.Sep 5, 1996 · N925UP · Boeing 72731C · Landing Gear DoorsSDR UPS96221039Stringer · corrodedINSPECTION TYPE-C, AFT CARGO COMPARTMENT CORROSION ON STRINGER 28L AT STA 990. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-3, 51-30-2.Aug 28, 1996 · N924UP · Boeing 72731C · Fuselage Main, Longeron/StringerSDR UPS96221038Actuator Rib · crackedINSPECTION TYPE-C, LT NR 2 SLAT ACTUATOR RIB MOUNT ON O/B SIDE IS CRACKED. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE PER SRM 57-50-2, 51-40-3, 51-30-1, 51-30-2, 51-10-1, 51-10-2.Aug 27, 1996 · N924UP · Boeing 72731C · Leading Edge Slat ActuatorSDR UPS96221040Frame · corrodedINSPECTION TYPE-C, AFT CARGO PIT STRINGER 28L AFT SIDE FRAME CHORD AT STA 990 HAS STRINGER ATTACH HOLE THAT IS CORRODED. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3.Aug 26, 1996 · N924UP · Boeing 72731C · Fuselage Main, FrameSDR UPS96221029Skin · crackedINSPECTION TYPE-C, 1 INCH CRACK IN LT WING NR 4 SLAT INTERNAL NEXT TO LAST I/B RIB ON I/B SIDE AT BOTTOM IN RADIUS 6 INCHES O/B OF RIB. STOP DRILLED CRACK/ FAB AND INSTALLED REPAIR DOUBLER.Aug 23, 1996 · N924UP · Boeing 72731C · Leading Edge DevicesSDR UPS96221028Clips · crackedINSPECTION TYPE-C, STA 1070 STR TO FRAME CLIPS CRACKED AT STR'S 5L, 6L, 7L. REMOVED AND REPLACED CLIPS PER BOEING DWG NR 65-45313.Aug 22, 1996 · N924UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS96221027Clips · crackedINSPECTION TYPE-C, STA 1070 STR TO FRAME CLIPS CRACKED AT STR'S 9R, 7R, 6R, 5R AND 4R. REMOVED AND REPAIRED CLIPS PER BOEING DWG NR 65-45313 AND SRM 51-30-2.Aug 22, 1996 · N924UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS96221026Clips · crackedINSPECTION TYPE-C, STA 1050 STR TO FRAME CLIPS AT 6R, 7R AND 9R. REMOVED AND REPLACED CLIPS PER BOEING DWG NR 65-45313 AND SRM 51-30-2-1.Aug 22, 1996 · N924UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS96221030Web · crackedINSPECTION TYPE-C, THE NR 1 SLAT ACTUATOR I/B ATTACH WEB CRACKED. REMOVED WEB DAMAGE AND FABRICATED REPLACEMENT WEB PER SB 727-57-0130, INSTALLED REPLACEMENT WEB PER SB 727-57-0130 AND SRM 51-30-2.Aug 20, 1996 · N924UP · Boeing 72731C · Leading Edge DevicesSDR UPS96220810Connector · wetON CLIMB-OUT FROM PHL, NR 1 ENGINE STRUT OVERHEAT LIGHT BEGAN FLICKERING. LIGHT BECAME STEADY UPON LEVEL OFF AT FL 280. ACCOMPLISHED ENGINE STRUT OVERHEAT QF CHECKLIST. LIGHT WENT OUT WHEN NR 1 THROTTLE RETARDED TO NEAR IDLE. AFTER ABOUT 5 MINS, LIGHT RE-IAug 6, 1996 · N925UP · Boeing 72731C · Overheat DetectionSDR UPS96220216Skin · corrodedINSPECTION TYPE: C. CORROSION ON EXTERIOR FUSELAGE SKIN ABOVE AFT CARGO DOOR. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW 53-10-1. REMOVED DAMAGED SKIN AND FABRICATED REPAIR PARTS IAW TRANCO EWO - 96-2307, SRM'S 53-30-0, 51-10-2, 51-20-1.May 26, 1996 · N922UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS96220213Bullnose Lugs · corrodedINSPECTION TYPE-C, NR 3 K-FLAP BULLNOSE LUGS CORRODED. REMOVED AND REPLACED NR 3 BULLNOSE IAW 57-51-21.May 21, 1996 · N922UP · Boeing 72731C · Leading Edge DevicesSDR UPS96220212Hinge Fitting · pittedINSPECTION TYPE-C, R/W NR 4 K-FLAP FIXED L/E CTR HINGE FITTING IS PITTIED. REMOVED AND REPLACED NR 4 K-FLAP CENTER HINGE FITTING IAW OHM 57-51-21.May 21, 1996 · N922UP · Boeing 72731C · Leading Edge DevicesSDR UPS96220211Bullnose Lugs · corrodedINSPECTION TYPE-C, NR 1 K-FLAP BULLNOSE LUGS CORRODED. REMOVED AND REPLACED BULLNOSE LUGS IAW M/M 27-81-01 AND OHM 57-51-01.May 21, 1996 · N922UP · Boeing 72731C · Leading Edge DevicesSDR UPS96220210Bullnose Lugs · corrodedINSPECTION TYPE-C, NR 2 K-FLAP BULLNOSE LUGS CORRODED. REMOVED AND REPLACED NR 2 K-FLAP BULLNOSE IAW OHM 57-51-21 AND M/M 27-81-01.May 21, 1996 · N922UP · Boeing 72731C · Leading Edge DevicesSDR UPS96220209Bulkhead Fitting · crackedINSPECTION TYPE-C, FOUND BULKHEAD FITTINGS TO BE CORRODED AND CRACKED STR 20R BS 1183 WL 190. REMOVED AND REPLACED CRACKED AND CORRODED FITTINGS STA 1183 STR 20R IAW 51-10-1, 51-10-2, 51-30-5.May 21, 1996 · N922UP · Boeing 72731C · Fuselage Main, BulkheadSDR UPS96220215Stringer · crackedINSPECTION TYPE-C, FOUND STRINGER 15R CRACKED AT SEVERAL LOCATIONS FROM STA 1125 TO 1180. REMOVED AND REPLACED STRINGER SECTION NR 15R STATION 1125 TO 1180 IAW 53-10-03.May 20, 1996 · N922UP · Boeing 72731C · Fuselage Main, Longeron/StringerSDR UPS96220214Skin · disbondedINSPECTION TYPE-C, RIGHT WING I/B AFT FLAP UPPER SIDE 17 O/B FROM I/B END AND 13 FWD FROM T/E IS DISBONDED. REMOVED DAMAGE AND REPAIRED DISBONDED IAW SRM 51-40-06.May 20, 1996 · N922UP · Boeing 72731C · Trailing Edge FlapsSDR UPS96220199Gate Beam · corrodedINSPECTION TYPE-C, CORROSION ON MID GALLEY LOWER GATE BEAM FORWARD SIDE INSIDE ON DOOR UNDER LEVELING COMPOUND STA 642, WL 217, RBL 69. CORROSION REMOVAL ON BEAM WAS OUT OF LIMITS, RELOCATED MID GALLEY LOWER GATE BEAM PER SRM 51-30-02.May 19, 1996 · N922UP · Boeing 72731C · Galley DoorsSDR UPS96220200Skin · corrodedINSPECTION TYPE-C, CORROSION ON INNER SKIN AT BS 705 TO 713, RBL 27 WL 153 UNDER RIGHT HAND WATER SEPARATOR. MECHANICALLY REMOVED CORROSION, REWORK OUT OF LIMITS IAW SRM 53-10-01 AND 53-30-01. REPAIRED SKIN STA 705 TO 713 RBL 27, WL 153, IAW SRM 53-30-03.May 18, 1996 · N922UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS96220202Beam · corrodedINSPECTION TYPE-C, CORROSION ON TOP DOGHOUSE BEAM AT BS 344, LBL 15. REMOVED AND REPLACED STIFFENER IAW SRM 51-30-02.May 17, 1996 · N922UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS96220201Shear Tie · corrodedINSPECTION TYPE-C, CORROSION ON SHEAR TIE AT BS 660 LBL 11 WL 150. REMOVED CORROSION, REWORK OUT OF LIMITS IAW SRM 53-10-01. REPAIRED FRAME SHEAR TIE STA 660 IAW SRM 51-40-03.May 17, 1996 · N922UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS96220195Fitting · crackedINSPECTION TYPE-C, CRACKED L-EXTRUSION AT RT FIN REAR SPAN CLOSURE RIB FITTING, ACCESS UNDER PANEL 9780. REMOVED AND REPLACED FITTING IAW SRM 51-30-2, 51-30-5.May 17, 1996 · N922UP · Boeing 72731C · Vertical StabilizerSDR UPS96220194Hat Channel · corrodedINSPECTION TYPE-C, CORROSION ON HAT CHANNEL AT STA 344, RBL 25 TO 35 WL 208. CORROSION REMOVAL OUT OF LIMITS, REMOVED CHANNEL, FABRICATED NEW PART, INSTALLED IAW SRM 53-10-1, 51-30-2.May 17, 1996 · N922UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS96220193Hat Channel · corrdedINSPECTION TYPE-C, CHANNEL AT BS 304 TO 344 RBL 17, WL 708 WAS FOUND TO BE CORRODED BEYOND LIMITS. REMOVED CORRODED HAT CHANNEL, FABRICATED NEW CHANNEL, REINSTALLED IAW SRM 53-10-01, 51-30-2.May 17, 1996 · N922UP · Boeing 72731C · Wing Miscellaneous StructureSDR UPS96220192Aileron Hinge · corrodedINSPECTION TYPE-C, R/W, O/B AILERON O/B CENTER HINGE FITTING IS CORRODED AILERON SIDE. REMOVED AND REPLACED R/W, O/B AILERON O/B CENTER HINGE FITTING ON AILERON SIDE IAW SRM 51-30-05, 51-30-02 OHM 20-50-03 AND M/M 57-50-11.May 16, 1996 · N922UP · Boeing 72731C · AileronsSDR UPS96220191Hinge · corrodedINSPECTION TYPE-C, R/W I/B AILERON CENTER AND O/B TAB HINGE FITTINGS ARE CORRODED AILERON SIDE. REMOVED AND REPLACED CENTER AND O/B TAB FITTINGS ON R/W, I/B AILERON IAW SRM 51-30-02.May 16, 1996 · N922UP · Boeing 72731C · AileronsSDR UPS96220190Skin · corrodedINSPECTION TYPE-C, CORROSION ON SKIN AT STA 1180 STR 7 LT WL 260. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1. REPAIRED SKIN AT STA 1180 STR 7 LT WL 260 IAW SRM 53-30-1.May 16, 1996 · N922UP · Boeing 72731C · Fuselage Main, Plate/SkinSDR UPS96220189Stiffener · corrodedINSPECTION TYPE-C, CORROSION ON TOP DOGHOUSE BEAM AT BS 336 LBL 15. REMOVED CORROSION, REWORKED OUT OF LIMITS IAW SRM 53-10-1, REMOVED AND REPLACED STIFFENER, BEAM IAW SRM 51-30-2.May 16, 1996 · N922UP · Boeing 72731C · Fuselage Miscellaneous StructureSDR UPS96205717Actuator · leakingCREW REPORTED AIR TURN BACK DUE TO A SYS HYDRAULIC FAILURE. TURN BACK AT 0457 Z, QUANTITY WENT TO ZERO. NR 5 KRUGER FLAP ACT. LEAKING, AWAITING PARTS FOR REPAIR.Mar 18, 1996 · N925UP · Boeing 72731C · Leading Edge Slat ActuatorSDR UPS205112Eel Assy · inoperativeWHILE ON GROUND, MAINTENANCE FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPS CHECK GOOD.Nov 29, 1995 · N922UP · Boeing 72731C · Emergency LightingSDR UPS205106Uplock Sw · out of positionCREW REPORTED AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT IN ACC WITH ADM PROCEDURES. THE GEAR WAS CYCLED AND IT STILL WOULD NOT RETRACT, BTB ACCOMPLISHED. RESEATED UPLOCK CHECK SWITCH ON CANNON PLUG PIN.Nov 20, 1995 · N925UP · Boeing 72731C · Landing Gear Position and WarningSDR UPS205103Eel Assy · inoperativeM/X DISCOVERED FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY, OPS CK GOOD. ON (P/N 10-0067-9) (S/N 9493), OFF (P/N 10-0067-9) (S/N 17745).Nov 20, 1995 · N926UP · Boeing 72731C · Emergency LightingSDR UPS205078Battery · looseWHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT INOP. FOUND BATTERIES LOOSE. TIGHTENED BATTERIES AND REINSTALLED EMERGENCY EXIT LIGHTS, OPS CK GOOD.Nov 15, 1995 · N926UP · Boeing 72731C · Emergency LightingSDR UPS504882Overheat Light · illuminatedCREW REPORTED AT TOP OF CLIMB AS THRUST WAS REDUCED, THE NR 2 ENGINE OVERHEAT LIGHT ON OVERHEAD PANEL FLICKERED FOR FIVE SECONDS THEN WENT OUT. ALL ENGINE INDICATIONS NORMAL EXCEPT ON EVM, THE NR 2 ENG N1 WAS AT .5, WHILE NR 1 AND NR 3 WERE .24. AT THE TOP OOct 26, 1995 · N924UP · Boeing 72731C · Engine Temperature Indicating SystemSDR UPS204882Wire · damagedSUPPLEMENTAL MRR: CREW REPORTED AT TOC AS THRUST WAS REDUCED, NR 2 ENG O/HEAT LIGHT ON OVERHEAD PANEL FLICKERED FOR 5 SECONDS AND WENT OUT. AT THE TOD DESCENT DURING THRUST REDUCTION, NR 2 ENG O/HEAT LIGHT CAME ON STEADY ILLUMINATING THE MASTER ENGINE O/HEATOct 25, 1995 · N924UP · Boeing 72731C · Engine Indicating System Wiring
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